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Shark UL User Manual
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Page 2-2
Flight manua
l
UL
aircraft
2.3.
ANALOG AIRS
PEED INDICATOR
MARKINGS
CAUTION:
All speeds in th
i
s m
anual are determ
ined
by
prim
ary airspeed
indicator disp
l
a
y
ed on EFI
S (Dynon Sk
y
View, FL
YMAP)
.
Ana
l
og
airspeed indicator
, used as em
ergency
one
,
m
ay
indica
te
slight
ly
different speeds
–
see item 5.1.
NORMAL
OPERATION
RANGE:
105
-
249
km/h
CAUTION
RANGE:
249
-
327
km/h
FLAPS
OPERATING
RANGE:
50
- 143
km/h
NEVER EXCE
E
D
SPEED:
327
m/h
15
17
Table of Contents
Default Chapter
7
Table of Contents
7
1 General
11
Introduction
11
Certification Bases
11
Warnings, Cautions and Notes
11
Airplane Basic Description
12
Three View Drawing
13
2 Limitations
15
Airspeed
15
Airspeed Indicator Markings
15
Analog Airspeed Indicator Markings
16
Engine
17
Engine Instrument Marking
18
Weight Limits
19
Center of Gravity (CG)
20
Approved Maneuvers
20
Maneuvering Load Factor G
20
Flight Crew
20
Kind of Operation
21
Fuel
21
Approved Fuel Types
21
Fuel Tanks Capacity
21
Other Limitations
22
Placards
23
3 Emergency Procedures
29
Engine Failure and Emergency Landing
29
Engine Failure During Take-Off Run
29
Engine Failure During Take-Off
29
In-Flight Engine Failure
30
Carburettor Icing
30
In-Flight Engine Restart
30
Fire
31
Engine Fire on the Ground
31
Engine Fire During Take-Off
31
Engine Fire in Flight
31
Cockpit / Electrical Fire
32
Gliding
32
Precautionary Landing
32
Blown-Out Tire Landing
32
Landing with Damaged Landing Gear
33
Landing Gear Retraction Malfunction
33
Landing Gear Opening Malfunction
33
Inadvertent Icing Encounter
34
Extreme Turbulence Encounter
34
Electrical System Malfunctions
35
Inadvertent Stall and Spin Recovery
36
Stall Recovery
36
Spin Recovery
36
Use of Rescue System
37
4 Normal Procedures
39
Pre-Flight Inspection
39
Cockpit
39
Wing
40
Landing Gear
40
Powerplant
40
Control Cables
41
Tail Unit and Fuselage
41
Turning on of Electric Devices
41
Engine Starting
41
Engine Warm-Up and Test
42
Before Taxiing
42
Taxiing
44
Check on Holding Line
44
Normal Take off
45
Climb
45
Cruise
46
Approach
46
Descent
46
Downwind
47
Normal Landing
47
On Base Leg
47
On Final
47
Landing
47
After Landing
48
Engine Shut down
48
Post-Flight Check
48
Short Field Take-Off and Landing Procedures
48
Balked Landing Procedures
48
Fuel SYSTEM Use
49
Repeated Take off
49
High Speed Flights
50
Turbulences
50
Maneuvering
50
Landing Gear Opening
50
Propeller, Engine RPM
51
Flaps
51
Landing Gear Retraction
51
Flutter, High Altitude Flights
51
5 Performance
53
Airspeed Indicator System Calibration
53
Stall Speed
54
TAKE-OFF Distance
54
In Flight Adjustable Prop. NEUFORM TXR2-V-70
54
In Flight Adjustable Prop. Woodcomp SR3000/2WN
55
On Ground Adjustable Prop. DUC SWIRL 1680
55
Landing Distance
56
Rate of Climb
56
Cruise, Endurance, Range
57
6 Airplane Empty Weight and COG Determination
61
Weight and Center of Gravity Determination for Flight
61
7 Technical Description of the Airplane
67
Airframe
68
Fuselage
68
Cockpit Canopy
68
Engine Cowlings
68
Wing
69
Ailerons
69
Flaps
69
Horizontal Stabilizer
69
Elevator
69
Rudder
69
Airplane Exterior Surface Painting
70
Landing Gear
70
Front Undercarriage
70
Main Undercarriage
71
Undercarriage Retraction and Extension
72
Control Systems
74
Elevator Control
74
Aileron Control
74
Rudder Control
75
Flaps
75
Elevator Trim Tab Control
75
Electric System
76
Fuel System
76
COCKPIT - Interior and Instruments
78
Power Unit
82
Technical Data
83
Propeller
84
DUC SWIRL 3 Blade, on the Ground Adjustable Propeller, Diameter 1680 MM
84
Woodcomp SR 3000 2W Two Blade in Flight Electrically Adjustable Propeller
85
Woodcomp KW 20W - Two Blade Hydraulically in Flight Adjustable
86
Neuform TXR2-V-70
87
Rescue System
88
Description of Rescue System Stratos/Junkers Magnum
88
The Activation Mechanism
89
Rescue System Installation
90
Towing System
91
Position Lights
92
Landing Light
92
ELT Unit
93
Autopilot
94
8 Airplane Handling, Care and Maintenance
95
Wing Dismounting
95
Remove Flaps
95
Disconnect Aileron Controls
96
Disconnect Rear Wing Spar Pin
96
Disassemble the Main Wing Spar Pins
96
Disconnect Fuel Hoses and Fuel Sensors Sockets
97
Remove Wing Spars out of Center-Wing
97
Disconnect Pitostatic System Hoses
97
Secure Wings by Hangaring (Transport) Jigs
97
Stabilizer Disassembly
97
Parking and Mooring
98
General
98
Cover of Pitot Tube
98
Mooring
98
Hangaring, Ground Handling
99
Towing
100
Tire Pressure
100
9 Supplements
101
5
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Shark UL Specifications
General
Brand
Shark
Model
UL
Category
Aircrafts
Language
English
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